Inlet tube design

ABSTRACT

A ram air fan assembly includes an outer housing. An inner housing is located within the outer housing. A motor is attached to the inner housing. An inlet tube extends between the outer housing and the motor. The inlet tube includes a straight first portion and a curved second portion. At least one of the two portions includes a perforated portion.

CROSS-REFERENCE TO RELATED APPLICATION(S)

This application is a divisional of application Ser. No. 14/261,905, nowU.S. Pat. No. 9,759,236, filed Apr. 25, 2014, and entitled INLET TUBEDESIGN, which is assigned to the same assignee as the presentapplication. Application Ser. No. 14/261,905 is hereby incorporated byreference.

BACKGROUND

The present invention relates to a ram air fan assembly. In particular,the invention relates to an inlet tube for a ram air fan assembly of anaircraft.

The environmental control system (“ECS”), including the ram air fanassembly, aboard an aircraft provides conditioned air to an aircraftcabin. Conditioned air is air at a desired temperature, pressure, andhumidity for aircraft passenger comfort. Compressing ambient air atflight altitude heats the resulting pressurized air sufficiently that itmust be cooled, even if the ambient air temperature is very low. Thus,under most conditions, heat must be removed from air by the ECS beforethe air is delivered to the aircraft cabin. As heat is removed from theair, it is dissipated by the ECS into a separate stream of air thatflows into the ECS, across heat exchangers in the ECS, and out of theaircraft, carrying the excess heat with it. Under conditions where theaircraft is moving fast enough, the pressure of air ramming into theaircraft is sufficient to move enough air through the ECS and over theheat exchangers to remove the excess heat.

While ram air works well under normal flight conditions, at lower flightspeeds, or when the aircraft is on the ground, ram air pressure is toolow to provide enough air flow across the heat exchangers for sufficientheat removal from the ECS.

Typically, ram air fan assemblies utilize an electric motor to drive thefan. This is accomplished by a rotor assembly, which is driven by astator. The stator generates a significant amount of heat as a byproductof the magnetic field used to drive the rotor assembly. Additionally,bearings that support the rotor assembly typically produce heat, andtherefore, require cooling. As a result of these sources of heat, theelectric motor must be cooled by sources such as external air. Thus, airis provided to the stator and bearings of the ram air fan along one ormore flow paths from upstream or downstream of the ram air fan in theECS.

Due to the collection inlet(s) location in the ECS (and the aircraft)adjacent the ram air fan assembly, the collection inlet(s) for coolingair are exposed to a high volume of particulate (such as dirt) duringoperation, which can result in foreign object damage (“FOD”). Thus, itis desirable to reduce the amount of particulate that reaches thosecomponents. Unfortunately, previous particle separators are ineffectiveat removing particulate from cooling air as previous particle separatorsrequire a high velocity clean airstream, which may not be available atthe ram air fan and the area there around. As a result, previousparticle separators are subject to problems such as clogging or operatein an undesirable manner by introducing particle laden cooling air tointerior components of the ram air fan.

SUMMARY

A ram air fan assembly includes an outer housing. An inner housing islocated within the outer housing. A motor is attached to the innerhousing. An inlet tube extends between the outer housing and the motor.The inlet tube includes a straight first portion and a curved secondportion. At least one of the two portions includes a perforated portion.

A method of filtration for use in a ram air fan assembly includesperforating a portion of an inlet tube with a plurality of perforations.A fan case is fluidly connected to a motor. Air flow is drawn throughthe inlet tube. A suction force of the air flow is then spread acrossthe perforated portion and a first end of the inlet tube.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a cross-sectional view of a ram air fan assembly.

FIG. 2A is a side elevation view of a j-tube of the ram air fanassembly.

FIG. 2B is a side elevation view of the j-tube of the ram air fanassembly.

DETAILED DESCRIPTION

The present invention relates to a ram air fan assembly. In particular,the invention relates to an inlet tube for a ram air fan assembly of anaircraft.

The inlet tube, or J-Tube, effectively separates particulates such asdirt from turbulent air flow passing adjacent the ram air fan andsupplies a flow of substantially clean cooling air to a motor stator andjournal bearings. The cooling passages are sized to operating conditionsand application specific parameters to draw air therein while leavingparticulate such as dirt to pass over the air inlet of the outer housingwithout entering the J-Tube. Once in the inner housing, the clean airflow passes through several elbow turns inside the inner housing beforeconnecting by a duct, hose, or similar passage to the ram air fan. Inthe ram air fan assembly, the clean cooling air flow is introduced byconventional means across the motor stator and the bearings. Theperforated J-Tube is advantageous because the unit can be positioned inparticle laden airflow and is able to achieve separation of unwantedparticles without experiencing negative side effects such as plugging orintroducing particle laden air to undesirable locations.

FIG. 1 shows a cross-section of ram air fan assembly 12 located withinECS 10. Ram air fan assembly 12 includes inner housing 14, inlet tube16, outer housing 18, bearing housing 20, fan rotor 22, motor rotor 24,motor stator 26, shaft 28, thrust plates 30, thrust bearings 32, journalbearings 34, terminal box 36, wire transfer tube 37, and inlet 38.

Outer housing 18 surrounds and encompasses bearing housing 20 and innerhousing 14. Outer housing 18 is attached to inner housing 14 at fanstruts. Bearing housing 20 is attached to inner housing 14 with bolts.Fan rotor 22 extends radially with respect to centerline C_(L) fromshaft 28 to adjacent outer housing 18 forward of bearing housing 20 andinner housing 14. In particular, fan rotor 22 is attached to shaft 28 byconventional means such as a tie rod (not numbered).

Motor rotor 24 and motor stator 26 are disposed within bearing housing20 and inner housing 14. In the embodiment shown, motor rotor 24 iscontained within motor stator 26 and connects to shaft 28. Together,motor rotor 24 and shaft 28 define an axis of rotation for ram air fanassembly 12.

Thrust plate 32 and inner housing 14 contain a flange extension of shaft28, with thrust bearings 32 positioned between the flange extension ofshaft 28 and thrust plate 32; and between the flange-like portion ofshaft 28 and inner housing 14. Journal bearings 34 are disposed aft ofthrust plate 32 and thrust bearings 32 and are positioned between shaft28 and bearing housing 20. Additionally, journal bearings 34 aredisposed along aft portion of shaft 28.

Terminal box 36 is disposed in outer housing 18 and electronics such aswires are run to inner housing 14 by wire transfer tube 37. Outerhousing 18 also contains inlet 38 which communicates with inner housing14 via inlet tube 16. As is illustrated in FIG. 1 with arrows A, coolingair flows from outer housing 18 to inner housing 14 through inlet 38,inlet tube 16, and additional ducts (not shown). Inlet 38 at the end ofinlet tube 16 is approximately 2.0-3.0 inches in diameter.

In the embodiment shown in FIG. 1, inlet tube 16 is positioneddownstream of fan rotor 22 (as defined by the direction of air flow witharrows A). The relative positioning of inlet tube 16 relative to theorientation of ram air fan assembly 12 is variable and is dictated byoperational specific criteria such as volume and velocity of air flow,estimated particle content, operational speeds of ram air fan, altitude,etc. Commercially available computational fluid dynamics software isavailable to aid in optimizing criteria such as the geometry andpositioning of inlet tube 16 given operational criteria.

Inlet tube 16 generally contains a shape resembling the letter J, and isoften referred to as a J-Tube. Inlet tube 16 may also include otherserpentine shapes which can include more than a single bend of 90degrees.

In operation, ram air fan assembly 12 is installed into ECS 10 aboard anaircraft and is connected to the fan inlet, the bypass inlet, and thefan outlet. When the aircraft does not move fast enough to generatesufficient ram air pressure to meet the cooling needs of ECS 10, poweris supplied to motor stator 26 to energize motor stator 26. This causesmotor rotor 24 to rotate about the axis of rotation for ram air fanassembly 12, rotating connected shaft 28 and fan rotor 22. Journalbearings 34 and thrust bearings 32 provide low friction support for therotating components. As fan rotor 22 rotates, it moves air in adownstream direction from the fan inlet, through outer housing 18 to thefan outlet.

Components within bearing housing 20 and inner housing 14, includingthrust bearings 32, journal bearings 34, motor stator 26, and motorrotor 24. These components generate significant heat and must be cooledduring operation. As previously discussed and illustrated in FIG. 1,cooling air is provided to flow across thrust bearings 32, journalbearings 34, motor stator 26, and motor rotor 24 and accomplish cooling.In particular, cooling air flows from outer housing 18 to inner housing14 through inlet 38, inlet tube 16 and additional ducts or passages (notshown). Once the cooling air has passed across thrust bearings 32,journal bearings 34, motor stator 26, and motor rotor 24 the air flowexits inner housing 14.

FIGS. 2A and 2B show side elevation views of inlet tube 16 of ram airfan assembly 12. Inlet tube 16 includes first portion 42 and secondportion 44. First portion 42 includes perforated portion 46. The shapeof first portion 42 includes a straight tubular shape. The shape ofsecond portion 44 includes a curved tubular shape.

Perforated portion 46 includes a plurality of perforations. Each of theplurality of perforations can have a diameter of approximately 0.1-0.2inches. The shape of each of the plurality of perforations may includecircular, hexagonal, elliptical, parallelogram, or other various uniformand non-uniform openings. The plurality of perforations on perforatedportion 46 allow for the same amount of air flow to enter into inlettube 16, but a suction force of the air flow is spread through all ofthe perforations and inlet 38 at the end of inlet tube 16. Thisspreading out of the air flow suction force decreases the amount offorce experience by foreign objects passing by inlet 38. Thissignificantly reduces the likelihood of foreign objects getting drawninto inlet tube 16 when the air flow enters ram air fan assembly 12.

Perforated portion 46 may extend the entire length of first portion 42.Alternatively, perforated portion 46 may extend along first portion 42for a distance less than the entire length of first portion 42. As shownin FIG. 2B, perforated portion 46 may also extend into second portion44.

Perforated portion 46 allows for air to be drawn into inlet tube 16 fromnot only the end of inlet tube 16, but also from inside fan outerhousing 18. Drawing air from within fan outer housing 18 reduces thesuction force of an inlet air flow that enters inlet 38. The reductionin the suction force of the inlet air flow also reduces the suctionforce experienced by FOD particles present in the air flow, thereforereducing the amount of FOD particles ingested into inlet 38. Anunperforated inlet tube creates a high suction force on the air flowentering the inlet. Any air flow entering into an engine through anunperforated inlet tube would contain a higher amount of FOD particlethan a perforated inlet tube, i.e. inlet tube 16, because the FODparticles would be subjected to a higher suction force drawing the FODparticles into inlet 38. The perforations of perforated portion 46 areunique in that they reduce suction pressures in the open end of inlettube 16, lessening the vacuuming effects of inlet 38 drawing swirlingFOD into inlet 38.

The plurality of perforations in perforated portion 46 also acts as afiltration for light FOD particulates in the stream of airflow thatenters ram air fan assembly 12. The rate of air flow also increases withthe presence of perforated portion 46 which provides more air flow tocool thrust bearings 32, journal bearings 34, motor stator 26, and motorrotor 24. Straight portion 42 extends approximately between 6.0-7.0inches. The perforations of perforated portion 46 are sized andpositioned so as not to receive particles from air flow passing throughinlet tube 16 such that only substantially clean air flow enters outerhousing 18 for cooling purposes.

Discussion of Possible Embodiments

The following are non-exclusive descriptions of possible embodiments ofthe present invention.

A ram air fan assembly includes an inner housing located within an outerhousing. A motor is attached to the inner housing. An inlet tube extendsbetween the outer housing and the motor. The inlet tube includes atleast a straight first portion and a second curved portion. At least oneof the straight first portion and the second curved portion includes aperforated portion.

The ram air fan assembly of the preceding paragraph can optionallyinclude, additionally and/or alternatively, any one or more of thefollowing features, configurations and/or additional components:

the perforated portion may comprise a plurality of uniformly spacedperforations;

each of the uniformly spaced perforations perforation may have adiameter of between about 0.1 and 0.2 inches (0.254 cm and 0.508 cm);

the perforated portion is may be disposed along the entire length of thestraight first portion of the inlet tube;

the perforated portion may be disposed along at least half of the lengthof the straight first portion of the inlet tube;

the perforated portion may be disposed along at least a portion of thecurved second portion of the inlet tube;

the inlet tube may have a diameter of between about 2.0 and 3.0 inches(5.08 cm and 7.62 cm);

a ratio of the inlet tube diameter to the diameter of each theperforations may be between 0.03 and 0.1;

a perforated portion may be disposed along the straight first portion ofinlet tube; and

the perforations are configured to allow a suction force of air to bespread across the plurality of perforations and a first end of the inlettube.

A method of filtration for use in a ram air fan assembly, the method mayinclude perforating a portion of an inlet tube with a plurality ofperforations, fluidly connecting a fan case with a motor with the inlettube, drawing an air flow through the inlet tube and spreading a suctionforce of the air flow across the perforated portion and a first end ofthe inlet tube.

a further embodiment of any of the foregoing method, wherein:

the air flow entering the inlet tube may be decreased;

an amount of foreign object ingestion into the inlet tube may beprevented;

the inlet tube may include a first straight portion and a second curvedportion, and perforating the inlet tube may include creatingperforations along an entire first straight portion of the inlet tube;

the inlet tube may include a first straight portion and a second curvedportion, and perforating the inlet tube may include creatingperforations along at least half of the straight first portion of theinlet tube; and

the inlet tube may include a first straight portion and a second curvedportion, and perforating the inlet tube may include creatingperforations along at least a portion of the curved second portion ofthe inlet tube.

While the invention has been described with reference to an exemplaryembodiment(s), it will be understood by those skilled in the art thatvarious changes may be made and equivalents may be substituted forelements thereof without departing from the scope of the invention. Inaddition, many modifications may be made to adapt a particular situationor material to the teachings of the invention without departing from theessential scope thereof. Therefore, it is intended that the inventionnot be limited to the particular embodiment(s) disclosed, but that theinvention will include all embodiments falling within the scope of theappended claims.

The invention claimed is:
 1. A method of cooling, the method comprising:drawing an air flow through a portion of an inlet tube of a ram air fanassembly, wherein the ram air fan assembly comprises: an outer housing;an inner housing located within the outer housing; and a motor attachedto the inner housing, wherein the inlet tube defines a portion of aflowpath leading to a downstream end of the inner housing and such thatthe inlet tube is fluidly connected to a downstream end of the motor,wherein the inlet tube comprises: an inlet; at least a straight firstportion; and a curved second portion, wherein the straight first portionand the curved second portion comprise a perforated portion withuniformly spaced perforations, wherein the perforated portion is fluidlyconnected to air within the outer housing; spreading a suction force ofthe air flow across the perforated portion and a first end of the inlettube.
 2. The method of claim 1, wherein the inlet tube is configured topull in ambient air.
 3. The method of claim 2, further comprisingpulling ambient air into the inlet tube.
 4. The method of claim 2,further comprising reducing a suction force of the air flow enteringinto the inlet of the inlet tube.
 5. The method of claim 2, furthercomprising drawing air flow from within the outer housing across theperforated portion and into the inlet tube.
 6. The method of claim 2,further comprising filtering particulate from the air flow entering intothe ram air fan assembly.
 7. The method of claim 2, further comprisingcooling the motor by flowing the air flow across at least one of thrustbearings, journal bearings, a motor stator, and a motor rotor of themotor.